A32X: Correct spoolup speed, fuel usage

This commit is contained in:
Joshua Davidson 2017-06-20 19:37:04 -04:00
parent 16b28e9cc0
commit e7d17877da
9 changed files with 18 additions and 18 deletions

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@ -2,8 +2,8 @@
<turbine_engine name="CFM56_5A1"> <turbine_engine name="CFM56_5A1">
<milthrust> 27000 </milthrust> <!-- Will put proper thrust amount once FDE sorted out --> <milthrust> 27000 </milthrust> <!-- Will put proper thrust amount once FDE sorted out -->
<bypassratio> 7.2 </bypassratio> <bypassratio> 8.1 </bypassratio>
<tsfc> 0.412 </tsfc> <tsfc> 0.5 </tsfc>
<bleed> 0.03 </bleed> <bleed> 0.03 </bleed>
<idlen1> 22.4 </idlen1> <idlen1> 22.4 </idlen1>
<idlen2> 60.9 </idlen2> <idlen2> 60.9 </idlen2>

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@ -2,8 +2,8 @@
<turbine_engine name="CFM56_5B3"> <turbine_engine name="CFM56_5B3">
<milthrust> 27000 </milthrust> <!-- Will put proper thrust amount once FDE sorted out --> <milthrust> 27000 </milthrust> <!-- Will put proper thrust amount once FDE sorted out -->
<bypassratio> 7.2 </bypassratio> <bypassratio> 8.1 </bypassratio>
<tsfc> 0.412 </tsfc> <tsfc> 0.5 </tsfc>
<bleed> 0.03 </bleed> <bleed> 0.03 </bleed>
<idlen1> 22.4 </idlen1> <idlen1> 22.4 </idlen1>
<idlen2> 60.9 </idlen2> <idlen2> 60.9 </idlen2>

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@ -2,8 +2,8 @@
<turbine_engine name="CFM56_5B4"> <turbine_engine name="CFM56_5B4">
<milthrust> 27000 </milthrust> <milthrust> 27000 </milthrust>
<bypassratio> 7.2 </bypassratio> <bypassratio> 8.1 </bypassratio>
<tsfc> 0.412 </tsfc> <tsfc> 0.5 </tsfc>
<bleed> 0.03 </bleed> <bleed> 0.03 </bleed>
<idlen1> 22.4 </idlen1> <idlen1> 22.4 </idlen1>
<idlen2> 60.9 </idlen2> <idlen2> 60.9 </idlen2>

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@ -2,8 +2,8 @@
<turbine_engine name="CFM56_5B6"> <turbine_engine name="CFM56_5B6">
<milthrust> 27000 </milthrust> <!-- Will put proper thrust amount once FDE sorted out --> <milthrust> 27000 </milthrust> <!-- Will put proper thrust amount once FDE sorted out -->
<bypassratio> 7.2 </bypassratio> <bypassratio> 8.1 </bypassratio>
<tsfc> 0.412 </tsfc> <tsfc> 0.5 </tsfc>
<bleed> 0.03 </bleed> <bleed> 0.03 </bleed>
<idlen1> 22.4 </idlen1> <idlen1> 22.4 </idlen1>
<idlen2> 60.9 </idlen2> <idlen2> 60.9 </idlen2>

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@ -2,8 +2,8 @@
<turbine_engine name="leap1a26"> <turbine_engine name="leap1a26">
<milthrust> 27000 </milthrust> <!-- Will put proper thrust amount once FDE sorted out --> <milthrust> 27000 </milthrust> <!-- Will put proper thrust amount once FDE sorted out -->
<bypassratio> 7.2 </bypassratio> <bypassratio> 8.1 </bypassratio>
<tsfc> 0.412 </tsfc> <tsfc> 0.5 </tsfc>
<bleed> 0.03 </bleed> <bleed> 0.03 </bleed>
<idlen1> 22.4 </idlen1> <idlen1> 22.4 </idlen1>
<idlen2> 60.9 </idlen2> <idlen2> 60.9 </idlen2>

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@ -2,8 +2,8 @@
<turbine_engine name="leap1a32"> <turbine_engine name="leap1a32">
<milthrust> 27000 </milthrust> <!-- Will put proper thrust amount once FDE sorted out --> <milthrust> 27000 </milthrust> <!-- Will put proper thrust amount once FDE sorted out -->
<bypassratio> 7.2 </bypassratio> <bypassratio> 8.1 </bypassratio>
<tsfc> 0.412 </tsfc> <tsfc> 0.5 </tsfc>
<bleed> 0.03 </bleed> <bleed> 0.03 </bleed>
<idlen1> 22.4 </idlen1> <idlen1> 22.4 </idlen1>
<idlen2> 60.9 </idlen2> <idlen2> 60.9 </idlen2>

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@ -2,8 +2,8 @@
<turbine_engine name="V2527_A5"> <turbine_engine name="V2527_A5">
<milthrust> 26600 </milthrust> <!-- Will put proper thrust amount once FDE sorted out --> <milthrust> 26600 </milthrust> <!-- Will put proper thrust amount once FDE sorted out -->
<bypassratio> 7.1 </bypassratio> <bypassratio> 10.1 </bypassratio>
<tsfc> 0.412 </tsfc> <tsfc> 0.5 </tsfc>
<bleed> 0.03 </bleed> <bleed> 0.03 </bleed>
<idlen1> 22.4 </idlen1> <idlen1> 22.4 </idlen1>
<idlen2> 60.9 </idlen2> <idlen2> 60.9 </idlen2>

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@ -2,8 +2,8 @@
<turbine_engine name="V2527_A5"> <turbine_engine name="V2527_A5">
<milthrust> 26600 </milthrust> <milthrust> 26600 </milthrust>
<bypassratio> 7.1 </bypassratio> <bypassratio> 10.1 </bypassratio>
<tsfc> 0.412 </tsfc> <tsfc> 0.5 </tsfc>
<bleed> 0.03 </bleed> <bleed> 0.03 </bleed>
<idlen1> 22.4 </idlen1> <idlen1> 22.4 </idlen1>
<idlen2> 60.9 </idlen2> <idlen2> 60.9 </idlen2>

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@ -2,8 +2,8 @@
<turbine_engine name="V2527_A5"> <turbine_engine name="V2527_A5">
<milthrust> 26600 </milthrust> <!-- Will put proper thrust amount once FDE sorted out --> <milthrust> 26600 </milthrust> <!-- Will put proper thrust amount once FDE sorted out -->
<bypassratio> 7.1 </bypassratio> <bypassratio> 10.1 </bypassratio>
<tsfc> 0.412 </tsfc> <tsfc> 0.5 </tsfc>
<bleed> 0.03 </bleed> <bleed> 0.03 </bleed>
<idlen1> 22.4 </idlen1> <idlen1> 22.4 </idlen1>
<idlen2> 60.9 </idlen2> <idlen2> 60.9 </idlen2>